US 5,526,292 AGranted

Broadband noise and vibration reduction

AssigneeLord Corporation

InventorsDouglas A. Hodgson, Mark R. Jolly, Mark A. Norris, Dino J. Rossetti, Douglas A. Swanson, Steve C. Southward

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Abstract

An active noise and vibration cancellation system with broadband control capability. A broadband disturbance signal detector positioned within a closed compartment such as an aircraft cabin or vehicle passenger compartment provides a signal representative of the frequency spectrum and corresponding relative magnitude of a broadband signal emanating from a vibrational energy source to a controller. The controller receives the broadband disturbance signal as well as error signals from error sensors which, by virtue of adaptive filters within the controller, enhance the cancellation capability of the control signals produced by one or more actuators positioned within the compartment.

Claims14

Dependent claims

A system for canceling vibrational energy within a passenger compartment comprising:

a) reference signal detecting means for sensing a frequency spectrum and corresponding relative magnitude of a broadband signal emanating from at least one vibrational energy source to which said compartment is exposed, said broadband signal including sound energy, said detecting means being situated in a key location with respect to said energy source to intercept said broadband signal on its way to said compartment;
b) error sensor means for detecting a residual internal level of vibrational energy within said compartment, said error sensor means being positioned down stream of said reference sensor detecting means;
c) actuator means placed to provide a control signal of appropriate frequency and magnitude to cancel some portion of said broadband vibrational signal, said actuator means including:
i) first actuator means producing a control signal spanning a first frequency range, and
ii) second actuator means producing a control signal spanning a second frequency range different from said first frequency range;
d) an adaptive controller including adaptive filters for generating broadband, time-domain command signals to activate said actuator means responsive to
i) said detecting means, and
ii) said error sensor means
to generate control signals of appropriate frequency and magnitude to destructively interfere with said broadband vibrational signal.

6 more elements

An active vibration control system for controlling broadband vibrational energy within a passenger compartment of an aircraft or the like, comprising:

a) reference sensor means for monitoring a broadband vibrational energy input signal to be controlled, said reference sensor means being positioned within said passenger compartment proximate a point of entry for said broadband vibrational energy input signal, said vibrational energy input signal having various spectral frequencies, said sensor means producing a reference signal which corresponds to said broadband vibrational energy input signal;
b) first actuator means for producing a first control signal for destructively interfering with at least a first portion of said broadband vibrational energy input signal, said first control signal spanning a first range of frequencies;
c) second actuator means for producing a second control signal for destructively interfering with at least a second portion of said broadband vibrational energy input signal, said second control signal spanning a second range of frequencies at least some of which are different from said first range of frequencies;
d) an adaptive controller including adaptive filter means for processing said reference signal and producing at least two actuator command signals, one each to said first and second actuator means, which are of appropriate frequency and magnitude to activate a respective said actuator means;
e) error sensor means for sensing a residual signal resulting from combining said first and second control signals with said input signal, and
f) circuitry means for feeding said residual signal back to said adaptive filter means to make adjustments in said actuator command signals.

3 more elements

An active vibration control system for controlling vibrational energy within a passenger compartment of an aircraft employing first and second active mounts for supporting respectively its first and second power plants comprising

a) first reference sensor means for monitoring a vibrational energy input signal to be controlled including at least one accelerometer mounted on said first power plant, said sensor means producing a first reference signal which corresponds to at least a portion of said vibrational energy input signal;
b) second reference sensor means for monitoring a vibrational energy input signal to be controlled including at least one accelerometer mounted on said second power plant, said sensor means producing a second reference signal which corresponds to at least a portion of said vibrational energy input signal;
c) first actuator means contained with said active mount for producing a first control signal reducing at least a first portion of said vibrational energy input signal by countering motion resulting from said first power plant;
d) second actuator means contained within said active mount for producing a second control signal reducing at least a second portion of said vibrational energy input signal by countering motion resulting from said second power plant;
e) an adaptive controller including adaptive filter means for processing said first and second reference signals and producing at least two actuator command signals, one each to said first and second actuator means, which are of appropriate frequency and magnitude to activate a respective said actuator means;
f) error sensor means for sensing a residual signal resulting from combining said first and second control signals with said vibrational energy input signal, and
g) circuitry means for feeding said residual signal back to said adaptive filter means to make adjustments in said actuator command signals.

4 more elements

Dependencies are inferred from the claim text.